EP2657135B1 - An aircraft black box - Google Patents

An aircraft black box Download PDF

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Publication number
EP2657135B1
EP2657135B1 EP11826142.9A EP11826142A EP2657135B1 EP 2657135 B1 EP2657135 B1 EP 2657135B1 EP 11826142 A EP11826142 A EP 11826142A EP 2657135 B1 EP2657135 B1 EP 2657135B1
Authority
EP
European Patent Office
Prior art keywords
aircraft
black box
crash
exhaust duct
duct
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP11826142.9A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2657135A2 (en
Inventor
Diego FOLCH CORTÉS
Eduardo VINUÉ SANTOLALLA
Enrique GUINALDO FERNÁNDEZ
Esteban MARTINO GONZÁLEZ
Pablo GOYA ABAURREA
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SL
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Airbus Operations SL
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Filing date
Publication date
Application filed by Airbus Operations SL filed Critical Airbus Operations SL
Publication of EP2657135A2 publication Critical patent/EP2657135A2/en
Application granted granted Critical
Publication of EP2657135B1 publication Critical patent/EP2657135B1/en
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0065—Black boxes, devices automatically broadcasting distress signals

Definitions

  • This invention refers to a black box installed in an aircraft and more in particular to a black box installed in a commercial aircraft.
  • Black boxes record, on one side, aircraft performance parameters and, on the other side, conversations between the pilot, ground control, copilot and other flight crew, as well as in certain cases images taken by cameras. Black boxes store only the information corresponding to a predetermined last period of the flight, typically 30 minutes.
  • Black boxes shall be crash survivable and easy to locate containers so they are designed to withstand a crash and they usually have automatic beacons which begin transmitting a signal after a crash to enhance their recoverability. They are usually installed in the tail zone of the aircraft, which provides crash protection for a typical crash. While black boxes can be easily recovered in crash events on land, the same does not apply to crash events in the sea where apart from the problem of locating the crashed aircraft there is the problem of recovering the black box in deep waters.
  • the present invention is oriented towards solving said drawbacks.
  • An object of the present invention is to provide an aircraft with a black box that can be easily recovered in an aircraft crash.
  • Another object of the present invention is to provide an aircraft with a black box that can be safely ejected outside the aircraft in a crash.
  • a commercial aircraft having a black box comprising a flight data recorder connected to suitable acquisition units for recording information required for crash investigation purposes inside a container, and in which:
  • the container has a rounded shape, which facilitates its ejection along tubular ducts.
  • said duct is an exhaust duct of an aircraft air conditioning system located in the rear part of the aircraft, and has its exit in a fuselage area subjected to negative aerodynamic pressure; the black box is installed over a frangible area of said exhaust duct; and the ejection means are suitable means for breaking or displacing said frangible area to allow the black box to fall into the exhaust duct.
  • said duct is an ad-hoc duct having inlet and outlet ways from/to the aircraft surface and doors for opening/closing said inlet and outlet ways; the black box is installed within said duct; and said ejection means are suitable means for opening simultaneously said doors.
  • the black box also comprises a location transmitting device using, preferably, a fuel cell as a source of energy and/or inflatable means and/or a parachute which are activated by said black box ejection control unit when an impending crash is detected by said crash detection device.
  • Figure 1 shows a black box 41 located in the rear zone of an aircraft 11 connected to data acquisition units 13, 14, 15 located in different areas of the aircraft and connected to the data sensors, sound sensor and/or image sensors needed for the black box 21 to record the information required for crash investigation purposes.
  • a typical black box 41 comprises (see Figure 2 ):
  • the black box 41 is installed inside the aircraft 11 over a frangible area of an exhaust duct 21 (typically a tubular duct) for evacuating exhaust gases in the direction indicated by arrow F1 located in the rear part of the aircraft fuselage so that in the event of a crash the black box 41 can be ejected through the exhaust duct 21 following the direction indicated by arrow F2.
  • an exhaust duct 21 typically a tubular duct
  • the black box 41 according to a preferred embodiment of this invention (see Figure 6 ) comprises at least a rounded-shaped container 43 such as an spherical container or an oval container for facilitating its ejection by a tubular duct, a flight data recorder 49 and a location transmitting device 51 including a switch device for its activation when the aircraft crash happens. Additionally, in preferred embodiments, it can comprise inflatable means 45 into the container 43 connected to a source of compressed gas which are designed as a black box floating means and/or as a black box impact resistant means and a parachute 47 into the container 43 designed as a black box impact resistant means.
  • a black box ejection control unit 19 activates, on one hand, an ejection means 23 that breaks or displaces the frangible area of the exhaust duct 21 to allow that the black box 41 falls into the exhaust duct 21, and on the other hand activates the location transmitting device 51 and, with a predetermined delay with respect to the activation of the ejection means 23, the inflatable means 45 and the parachute 47, if present, so that they can initiate its deployment.
  • the black box 41 In a second embodiment of the present invention illustrated in Figures 7, 8, 9 and 10 the black box 41, having the same elements than in the first embodiment, is installed inside the aircraft 11 within an ad-hoc duct 31 located in an aircraft area where the risk that the ejected black box can impact on the aircraft is minimum to facilitate its ejection.
  • the duct 31 has inlet and outlet ways 33, 35 with doors 37, 39 so that in the event of a crash detected by the detecting means 17 the ejection control unit 19 activates the ejection means 33 that open simultaneously said doors 37, 39 so that an external airflow can enter into the duct 31 by the inlet way 33 as indicated by arrow F1 causing an impact on the black box 41 due to dynamic pressure inside the duct 31 forcing it to be ejected outside of the aircraft through the outlet way 35 following the direction indicated by arrow F2.
  • the activation of the ejection means triggers the activation of the location transmitting device 51 as well as the inflatable means 45 and/or the parachute 47, if present, so that they can initiate its deployment.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Toys (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Emergency Lowering Means (AREA)
  • Recording Measured Values (AREA)
  • Traffic Control Systems (AREA)
EP11826142.9A 2010-12-22 2011-12-16 An aircraft black box Active EP2657135B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES201031920A ES2403954B1 (es) 2010-12-22 2010-12-22 Una caja negra de una aeronave.
PCT/ES2011/070874 WO2012085314A2 (es) 2010-12-22 2011-12-16 Una caja negra de una aeronave

Publications (2)

Publication Number Publication Date
EP2657135A2 EP2657135A2 (en) 2013-10-30
EP2657135B1 true EP2657135B1 (en) 2016-09-28

Family

ID=45852563

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11826142.9A Active EP2657135B1 (en) 2010-12-22 2011-12-16 An aircraft black box

Country Status (5)

Country Link
US (1) US8489259B2 (zh)
EP (1) EP2657135B1 (zh)
CN (1) CN103269952B (zh)
ES (1) ES2403954B1 (zh)
WO (1) WO2012085314A2 (zh)

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US20140257602A1 (en) * 2013-03-06 2014-09-11 Gulfstream Aerospace Corporation Methods and systems for instructing an aircraft to perform a go-around maneuver
US8706357B1 (en) * 2013-03-14 2014-04-22 Drs C3 & Aviation Company Flight recorder deployment system and method
US9296489B2 (en) 2013-03-14 2016-03-29 Drs C3 & Aviation Company Flight recorder deployment mechanism
FR3013032B1 (fr) * 2013-11-12 2017-07-21 Airbus Operations Sas Balise de detresse integree a l'empennage vertical d'un aeronef
CN103646442B (zh) * 2013-11-28 2015-12-02 陕西千山航空电子有限责任公司 一种具有嗅觉定位功能的航空记录器
CN104139859A (zh) * 2014-05-12 2014-11-12 中国航空工业集团公司沈阳飞机设计研究所 一种水上漂浮记录器弹射方法
CN104007451B (zh) * 2014-05-27 2016-06-08 曹宇 遇难位置记录报告装置
CN104135258B (zh) * 2014-06-17 2017-03-08 中国航空工业集团公司沈阳飞机设计研究所 一种水上漂浮记录器防误触发装置及方法
US9767692B1 (en) 2014-06-25 2017-09-19 Louvena Vaudreuil Vehicle and environmental data acquisition and conditioned response system
US10713859B1 (en) * 2014-09-12 2020-07-14 World Wide Walkie Talkie (Mbt) Wireless flight data recorder with satellite network method for real time remote access and black box backup
US9452844B1 (en) 2015-03-05 2016-09-27 Comac America Corporation Emergency mechanical and communication systems and methods for aircraft
CN105139480A (zh) * 2015-08-10 2015-12-09 昆明五威科工贸有限公司 一种黑匣子系统的定位方法
CN105253306A (zh) * 2015-11-09 2016-01-20 杨珊珊 一种设置有坠落保护装置的无人飞行器及其坠落保护方法
IL246554B (en) * 2016-06-30 2021-10-31 Israel Aerospace Ind Ltd A system is deployed to support emergency situations
CN106347689A (zh) * 2016-08-28 2017-01-25 桂林市晶准测控技术有限公司 一种黑匣子分离控制方法、系统和航空器
CN106364681A (zh) * 2016-08-28 2017-02-01 桂林市晶准测控技术有限公司 一种抛放式黑匣子
CN106143929A (zh) * 2016-08-28 2016-11-23 桂林市晶准测控技术有限公司 一种抛放式黑匣子弹射控制方法、系统和航空器
CN106379545A (zh) * 2016-08-30 2017-02-08 陕西千山航空电子有限责任公司 一种具有减速功能的抗毁抛放记录器
CN106167097A (zh) * 2016-08-30 2016-11-30 陕西千山航空电子有限责任公司 一种机载抛放记录器弹射方法
CN106347690B (zh) * 2016-09-01 2019-11-08 肇庆高新区异星科技有限公司 一种黑匣子控制方法及系统
US10424138B2 (en) 2016-11-23 2019-09-24 International Business Machines Corporation Detachable drone for monitoring a moving vessel
WO2018098774A1 (zh) * 2016-12-01 2018-06-07 深圳市大疆创新科技有限公司 一种控制迫降的装置、方法、设备
US9738398B1 (en) 2017-01-27 2017-08-22 Comac America Corporation Ejectable flight data recorder systems, methods, and devices
GB2559757A (en) 2017-02-16 2018-08-22 Airbus Operations Ltd Ejectable flight data recorder unit
FR3073675B1 (fr) * 2017-11-14 2019-10-04 Safran Power Units Systeme de generation d'energie electrique nomade pour un aeronef comprenant une pile a combustible
DE102018007062A1 (de) * 2018-09-06 2020-03-12 Airbus Operations Gmbh Notlokalisierungsgerät, insbesondere ELT, zum Auslösen einer Notfallmaßnahme
DE102018008418B4 (de) * 2018-10-26 2021-09-23 Henryk Bastian Datenspeichereinrichtung für schnelle Ortung und Lokalisierung des Datenspeicherelements für Flugzeuge
US10803684B2 (en) 2018-10-31 2020-10-13 Honeywell International Inc. Aircraft systems and methods for retrospective pilot input analysis
CN110015439B (zh) * 2019-04-15 2022-03-29 中北大学 一种飞行器黑匣子的回收方法及飞行器黑匣子回收装置
CN111498113B (zh) * 2020-05-06 2022-12-23 中国商用飞机有限责任公司 抛放式飞行记录器系统和控制方法
CN111907707B (zh) * 2020-06-15 2021-09-07 哈尔滨工业大学 一种电磁驱动的黑匣子抛放机构
CN112874795A (zh) * 2021-01-21 2021-06-01 北京京东乾石科技有限公司 抛射装置、无人机、控制方法、装置及存储介质
CN113886998B (zh) * 2021-12-07 2022-03-08 中国科学院工程热物理研究所 一种多层球结构的设计方法

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ES2303773B1 (es) * 2007-02-01 2009-05-01 Fco. Javier Garcia Barrientos Sistema de recuperacion y salvamento para aeronaves.

Also Published As

Publication number Publication date
WO2012085314A2 (es) 2012-06-28
ES2403954A2 (es) 2013-05-22
ES2403954B1 (es) 2014-04-29
US8489259B2 (en) 2013-07-16
WO2012085314A3 (es) 2012-09-07
US20120166037A1 (en) 2012-06-28
CN103269952A (zh) 2013-08-28
ES2403954R1 (es) 2013-05-24
CN103269952B (zh) 2016-04-06
EP2657135A2 (en) 2013-10-30

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